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Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  Favorite  |  View/Download：345/101  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  Favorite  |  View/Download：129/2  |  Submit date：2023/03/23
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download：296/65  |  Submit date：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model 期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 193, 页码: 246-256
Authors:  Yang PF;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
View  |  Adobe PDF(2840Kb)  |  Favorite  |  View/Download：793/131  |  Submit date：2018/10/30
Oblique detonation  Induction-reaction kinetics  Initiation length  Initiation structure  
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture 期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
Authors:  Wang T;  Zhang YN;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD;  Wang, T (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1388Kb)  |  Favorite  |  View/Download：438/141  |  Submit date：2016/01/08
Evolution of cellular structures on oblique detonation surfaces 期刊论文
COMBUSTION AND FLAME, 2015, 卷号: 162, 期号: 2, 页码: 470-477
Authors:  Teng HH(滕宏辉);  Ng HD;  Li K(李康);  Luo CT(罗长童);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1555Kb)  |  Favorite  |  View/Download：3276/867  |  Submit date：2015/03/17
Detonation  Instability  Cellular Structure  Transverse Wave  Numerical Simulations  
Numerical investigation on the induction zone structure of the oblique detonation waves 期刊论文
Computers & Fluids, 2014, 卷号: 95, 页码: 127-131
Authors:  Teng HH(滕宏辉);  Zhang YN;  Jiang ZL(姜宗林);  Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1128Kb)  |  Favorite  |  View/Download：1039/277  |  Submit date：2014/06/19
Detonation  Oblique Shock  Induction  Unstationary  
Numerical simulation of deflagration to detonation transition in a straight duct: Effects of energy release and detonation stability 期刊论文
Advances in Applied Mathematics and Mechanics, 2014, 卷号: 6, 期号: 6, 页码: 718-731
Authors:  Dou HS;  Hu ZM(胡宗民);  Khoo BC;  Jiang ZL(姜宗林)
View  |  Adobe PDF(487Kb)  |  Favorite  |  View/Download：841/258  |  Submit date：2014/11/27
Numerical Simulation  Detonation  Ddt  Energy Release  Duct  
边界层对驻定斜爆轰结构和稳定性的影响 期刊论文
科学技术与工程, 2013, 卷号: 13, 期号: 23, 页码: 6781-6787
Authors:  王爱峰;  滕宏辉;  赵伟;  姜宗林
Adobe PDF(4286Kb)  |  Favorite  |  View/Download：782/264  |  Submit date：2013/10/11
边界层  驻定斜爆轰  稳定性  流场结构  高超声速  
A reconstructed discontinuous Galerkin method based on a Hierarchical WENO reconstruction for compressible flows on tetrahedral grids 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2013, 卷号: 236, 页码: 477-492
Authors:  Luo H;  Xia YD;  Spiegel S;  Nourgaliev R;  Jiang ZL(姜宗林);  Luo, H (reprint author), N Carolina State Univ, Dept Mech & Aerosp Engn, Raleigh, NC 27695 USA.
Adobe PDF(2739Kb)  |  Favorite  |  View/Download：1396/508  |  Submit date：2013/03/25
Discontinuous Galerkin Method  Weno Reconstruction  Unstructured Grids